Presentation - The 5th Nano
Transcription
Presentation - The 5th Nano
Nagoya, Japan 10-13 October 2012 Research and Application Based Space Education A.Rüstem ASLAN1), Rei KAWASHIMA2), M. Khalil IBRAHIM3) 1) Astronautical Engineering, Istanbul Technical University, Istanbul, Turkey 2) University Space Engineering Consortium, Tokyo, Japan 3) Department of Aerospace Engineering, Cairo University, Giza, Egypt [email protected] Decade of Education for Sustainable Development (DESD) • 12/2002, the UN GA resolution 57/254 a UN DESD, from 2005 to 2014. • Basic vision: A world where everyone has the opportunity to benefit from education and learn the values, behaviors and lifestyles required for a sustainable future and for positive societal transformation. Space Technologies • contribute significantly to wealth creation and quality of life, both directly and in terms of technology spin-off to other sectors. • Increasing number of citizens involved in space education and related work (cutting edge technology) is of paramount importance for the benefit and wealth of world’s people. CubeSats/NanoSats • CubeSats made space within reach of everybody regardless of budget and extensive know-how. • Small budgets and short development times. • Great educational tool, involve everybody in high tech work, increase national and international cooperation and collaboration for a safer peacefull world. UNISEC of Japan • UNISEC member universities are supporting education using CanSat at high school level. • Many educators at university level have addressed the effectiveness of hands-on training, because it provides unique opportunities and students can learn project management skills as well as technical process of space projects. • UNISEC activities would enable those in teaching positions at universities to improve their teaching skills as well as their academic performance and output. Japanese history of university micro/nano satellite activities UNISEC of Japan • MIC1-2 • CLTP 1-2-3 • UNISEC-INT • Turkey, Egypt, others CLTP CLTP 1 Period Feb-March 2011 2 Nov-Dec 2011 3 July-August 2012 Host university Wakayama Univ. Participating countries Algeria, Australia, Egypt, Guatemala, Mexico, Nigeria, Peru, Sri Lanka, Turkey(3) and Vietnam Indonesia, Malaysia, Nigeria, Vietnam, Ghana, Peru, Nihon Univ. Singapore, Mongolia, Thailand and Turkey Brazil, Egypt(2), Israel, Tokyo Lithuania, Namibia, Nigeria, Metropolitan Mongolia, Philippines and University Turkey CLTP2 TURKISH CASE ITU, Space Engineering • Establishment 1983 (ITU 1773) • 60 new students per year • Space related labs – Spacecraft Systems Design and Testing – Small Satellite communication • Aim: – Research and testing on nano satellites and small sat components – To have engineers with laboratory experience to serve the national aerospace industry Space Engineering Curriculum • • • • Education in space science and technologies Follows AIAA recomendations Fully Accredited by ABET till 2017 Space related undergraduate courses – – – – – – – – Introduction to Space Engineering (1st year) Aerospace structures (3rd year) Orbital Mechanics, (3rd year) Space environment, (4th year) Spacecraft Attitude Determination and Control (4th) Rocket and Electric Propulsion (4th) Spacecraft system design with application (SSD) (4th) Spacecraft communications (4th) Curriculum (AIAA/ABET) • ‘’Astronautical engineering programs must demonstrate that graduates have knowledge of orbital mechanics, space environment, attitude determination and control, telecommunications, space structures, and rocket propulsion’’. • ‘’Program must also demonstrate that graduates have design competence that includes integration of astronautical topics’’. • (http://www.aiaa.org/content.cfm?pageid=472 Spacecraft System Design • Last semester required course • Capstone design project • Conceptual design, no time for a prototype • Topic: AIAA SDC, MIC, other Design- Development phases Test & Integration Satellite Infrastructure / Payloads / Systems Thermal Vacuum, Vibration, EMC Design / Analysis / Production Ground Station •Conceptual design •Desktop model •Engineering model •Flight Model Istanbul Technical University - Faculty of Aeronautics and Astronautics http://usl.itu.edu.tr SSD 2011: Space Debris Removal at LEO (AIAA SDC) Educational aspect of MIC! • MIC1 evaluation comittee comment: – only experienced applicants with some space background and national heritage are succesful in the finals. A general summary of finalist teams in MIC1 and MIC2: • Experienced team • Connection to a lab or group • Ongoing work not just a new idea to be realized • Not undergraduate students • Some pratical work already done MIC2 Turkish Case (10 applicants no finalist or semi finalist) • Only undergraduate students (SSD topic) or MS with no space background at all. • Mostly Non-interdisciplinary teams (just space engineers) • Just a limited time: 3 months to find an idea and to implement it although the MIC time is longer • Finding an idea is a good element, reading many different papers on different topics • No time to implement or to evaluate the suitability of the idea • 2 term course work may be a remedy MIC vs AIAA for SSD MIC AIAA Written for Written for everyone (undergraduate) students Comment Success requires prior experience in the field, professionals have more chance of winning the contest Mission is broadly specified Request For Proposal (RFP) is not available Mission is given, Student directly starts design based solution is sought on given mission, requirements and A clear and detailed constraints RFP is given Mission idea sought Solution to a given mission is sought Students spend considerable time to find an idea, little time left to design for the idea Student team structure is possible Student Team structure ony AIAA for US students only Professional Development of Students • insufficient applied course work • Student Clubs (UUMK, EUROAVIA, AIAA, PARS...) • Extracurricular activities – Own will – İnterdisciplinary team work – International collaborations – Employment advantages Extracurricular activities actual applications • International students competitions: – AIAA/DBF, – CanSat, – UAVSI, – AHS, – AIAA-ASMA/IGTI Engine Design – Solar Car and Boat – MIC • CubeSat Projects International competitions ITU SE CubeSat Projects TURKSAT 3USAT ITUPSAT1 UHF DOWNLINK VHF UPLINK W NL IN K UH F DO VH EHF SAT FU PL IN K UYDU QB50: BeeagleSat YER ISTASYONU - 1 YER ISTASYONU - 2 Project Comparison • • • • • • • • • • • ITUpSAT1 One unit CubeSat 25 Project Personnel Mainly space engineers 19 Space, 5 Electronics, 1 Mechanical Engineer No redundancy 3 year development time Infrastructure development Budget: ITU and TUBITAK Some undergraduate, MS thesis Empleoyment by the industry • • • • • • • • • • • TURKSAT-3USAT Three unit CubeSat 50 project personnel Interdisciplinary team work 24 Aerospace,2 Mechanical 24 ElectricElectronics Full redundancy 2 year development time TAMSAT Engineers Budget: TÜRKSAT Inc. Many undergraduate, MS thesis Empleoyment by the industry Evolvement • ITUpSAT1: 1 department, governement support, MS students, thesis, hands on experience • 3USAT: 3 departments, company and public support. BS and MS thesis, hands on experience • QB50: 3 universities, many departments, industry support. • EHFSAT: Payload by the industry, SME support (spin-off company), 3 departments. Research and Application Based Space Education: Egyptian Case Mohammed Khalil Ibrahim, Ph.D. Space Systems Technology Laboratory Aerospace Engineering Department Cairo University - Egypt Background • Faculty of Engineering, Cairo University Established in 1820. • Aerospace Engineering Department established in 1938. • Egyptian Space Program is running by NARSS (1999 ) • B.Sc. in Space Engineering is Elective • Ph.D. & M.Sc. in Space Engineering • Lack of Practical Space Engineering Projects. Laboratories & Facilities • • • • • • Aerodynamics Flow Visualization Aircraft Propulsion Aircraft Structure Automatic Control & Flight Mechanics Space Systems Technology established in 2011 31 CanSat-Based Space Engineering • Bi-annual practical space engineering training course for all students from 2011 . • Mandatory summer training course for Junior students from 2013 . CanSat-Based Space Engineering CanSat Based-Space Engineering Education Mechanical Design and Production Parachute Aerodynamics Launcher Development Microcontroller, MEMS sensors and Firmware Development Basic Electronic Circuits System Engineering Project Management Advanced CanSat Project • Rover-Back CanSat • Fully Autonomous • Schedule to Join Arliss 2013 Oct-11 Nov Dec Jan 12 Feb Mar Apr May Jun Jul Aug Sep Oct 1st & 2nd Conceptual Models (CM) 3rd CM EM FM Number of Submitted Idea MIC Participations 8 Category1 Category2 6 4 2 0 MIC-1 MIC-2 MIC1: Total Number of Submitted Idea is 62 MIC2: Total Number of Submitted Idea is 54 (Cat.1) and 20 (Cat. 2) R&D Projects • Advanced CanSat • Development of Simple Ground Station • CanSat Launcher – QuadRotor – Balloon • CubeSat Subsystems – – – – – – Communication C&DH ADCS Payload Structure EPS Students Enrollment • Faculty of Engineering, Cairo University receive top 5% Senior High-School Students (3000 students/year). • Total of 15000 Undergraduate Students. • Aerospace Engineering Department Receive 100 students/year. • Total of 400 Undergraduate Students in Aerospace Engineering Department. Faculty of Engineering (2012) 8 7 6 5 4 3 2 1 0 % Grade Ranking Aerospace Engineering 2009 2010 2011 Academic Year 2012 80 70 60 50 40 30 20 10 0 Benefits-Education • Space project: higly motivated students, individuals • Applied education: plan, design, produce, test, integrate, launch, observe a spacequalified actual satellite during education • Multidisciplinary research teams at universities • Establish design, manufacturing and testing infrasturcture • Raise qualified and experienced Space Engineers for aerospace industry • Increase national capability in satellite technologies Benefits • Accounting for space debris in project planning, compliance with UN regulations • A new job sector: entrepreneurship, student owned SMEs, Pumpkin, ISIS, Clyde Space, Gumush • To reach space is a realm of possibility for everyone... Conclusions • Practical project work and design studies are important elements of space education. • CanSat and CubeSat programs have a positive effect on increasing space awareness particularly among students with international interaction. • MIC and CLTP are useful tools Conclusions • Clearly defined topics seems to be more suitable for high school and undergraduate university programs • Open end projects may be successfully undertaken by experienced graduate students and space professionals. • All these developments have started to shape space education curriculum, worldwide. • How can we benefit further from extracurricular activities to enhance space education curriculum? Acknowledgments • the Nano-Satellite Symposium Office and The Basic Space Technology Initiative (BSTI) of the United Nations Program on Space Applications Acknowledgments • "HODOYOSHI Project" that enabled CLTP and MIC to launch, which was granted to Prof. Shinichi Nakasuka by the Japan Society for the Promotion of Science in the "Funding Program for World-Leading Innovative R&D on Science and Technology (FIRST Program)," initiated by the Council for Science and Technology Policy of the Cabinet Office, Government of Japan. ITUpSAT1, 3rd year in orbit TURKSAT-3USAT MISSION 3USAT UHF DOWNLINK VHF UPLINK UH F DO VH W NL IN K FU PL IN K UYDU YER ISTASYONU Ground Station- 11 YER ISTASYONU - 22 Ground Station TURKSAT-3USAT • 3U CubeSat • VHF/UHF linear Transponder • Redundant design, back-up systems designed, developed, manufactured and tested in Turkey • Cutting edge de-orbiting and power system QB50: BeEagleSat EHF-SAT YER ISTASYONU – 1 Ground Station 1 Telemetri, Telemetry, telecommand telekomand X-Band DOWNLINK Ku Band UPLINK UH F DO VH W NL IN K FU PL IN K EHF-SAT UYDU YER ISTASYONU –2 2 Ground Station Transponder Transponder AEROSPACE PROJECTS KARAYEL DRT ITUpSAT1 HTH MILGEM HELSIM ANKA RIHA1A RIHA1B İTÜ-HTH Tüm alt sistemleri ile, Temmuz 2011, TAI, Ankara UNISEC-EGYPT • Seminar and Panel Discussion about establishing UNSEC-Egypt (July 4, 2012) • Next meeting scheduled to be in Feb. 2013. Pros and Cons of Establishing UNISEC-Egypt Pros Cons Space awareness expansion Lack of team-work experince Well managed capacity building plans Dedicated management board Resource management Legal entity Large scale space projects Sustainable Funding QB50 - THE IDEA • An international network of 50 double CubeSats for multi-point, in-situ, long-duration measurements in the lower thermosphere and for re-entry research • A network of 50 double CubeSats sequentially deployed (1 CubeSat every orbit or every 2 or 3 orbits) • Initial altitude: 330 km (circular orbit, i=79°) • Downlink using the Global Educational Network for Satellite Operations (GENSO) 58 von Karman Institute for Fluid Dynamics
Similar documents
Presentation - The 5th Nano
ITU, TurAFA and SU along with national space industry benefit from QB50. A 2U CubeSat with sensor Set 3 is being developed. A local X-Ray detector will be space tested. Students, through hands-on w...
More information